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Artigo de periodico
Power extraction from stall-induced oscillations of an airfoil (2018)
Marques, Flavio Donizeti ; Pereira, Daniel Almeida; Zakaria, Mohamed Y.; Hajj, Muhammad R
Source: Journal of Intelligent Material Systems and Structures. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, ENERGIA, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARQUES, Flavio Donizeti et al. Power extraction from stall-induced oscillations of an airfoil. Journal of Intelligent Material Systems and Structures, v. 29, n. 7, p. 1407-1417, 2018Tradução . . Disponível em: https://doi.org/10.1177/1045389X17739161. Acesso em: 30 abr. 2024.
APA
Marques, F. D., Pereira, D. A., Zakaria, M. Y., & Hajj, M. R. (2018). Power extraction from stall-induced oscillations of an airfoil. Journal of Intelligent Material Systems and Structures, 29( 7), 1407-1417. doi:10.1177/1045389X17739161
NLM
Marques FD, Pereira DA, Zakaria MY, Hajj MR. Power extraction from stall-induced oscillations of an airfoil [Internet]. Journal of Intelligent Material Systems and Structures. 2018 ; 29( 7): 1407-1417.[citado 2024 abr. 30 ] Available from: https://doi.org/10.1177/1045389X17739161
Vancouver
Marques FD, Pereira DA, Zakaria MY, Hajj MR. Power extraction from stall-induced oscillations of an airfoil [Internet]. Journal of Intelligent Material Systems and Structures. 2018 ; 29( 7): 1407-1417.[citado 2024 abr. 30 ] Available from: https://doi.org/10.1177/1045389X17739161
Trabalho de evento
Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils (2017)
Pereira, Daniel Almeida; Santos, Carlos Renan dos ; Marques, Flavio Donizeti
Source: Proceedings. Conference titles: International Symposium on Dynamic Problems of Mechanics - DINAME. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
PEREIRA, Daniel Almeida e SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti. Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils. 2017, Anais.. Rio de Janeiro, RJ: ABCM, 2017. Disponível em: https://repositorio.usp.br/directbitstream/2944c4eb-e02f-4c63-968d-6fe84db91245/PROD_25662_SYSNO_3123990.pdf. Acesso em: 30 abr. 2024.
APA
Pereira, D. A., Santos, C. R. dos, & Marques, F. D. (2017). Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils. In Proceedings. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/2944c4eb-e02f-4c63-968d-6fe84db91245/PROD_25662_SYSNO_3123990.pdf
NLM
Pereira DA, Santos CR dos, Marques FD. Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils [Internet]. Proceedings. 2017 ;[citado 2024 abr. 30 ] Available from: https://repositorio.usp.br/directbitstream/2944c4eb-e02f-4c63-968d-6fe84db91245/PROD_25662_SYSNO_3123990.pdf
Vancouver
Pereira DA, Santos CR dos, Marques FD. Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils [Internet]. Proceedings. 2017 ;[citado 2024 abr. 30 ] Available from: https://repositorio.usp.br/directbitstream/2944c4eb-e02f-4c63-968d-6fe84db91245/PROD_25662_SYSNO_3123990.pdf
Trabalho de evento
Nonlinear airfoil torsional response induced by separated flows (2015)
Pereira, Daniel Almeida; Vasconcellos, Rui Marcos Grombone de; Marques, Flavio Donizeti
Source: Proceedings. Conference titles: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
PEREIRA, Daniel Almeida e VASCONCELLOS, Rui Marcos Grombone de e MARQUES, Flavio Donizeti. Nonlinear airfoil torsional response induced by separated flows. 2015, Anais.. Reston, VA: AIAA, 2015. Disponível em: https://doi.org/10.2514/6.2015-1423. Acesso em: 30 abr. 2024.
APA
Pereira, D. A., Vasconcellos, R. M. G. de, & Marques, F. D. (2015). Nonlinear airfoil torsional response induced by separated flows. In Proceedings. Reston, VA: AIAA. doi:10.2514/6.2015-1423
NLM
Pereira DA, Vasconcellos RMG de, Marques FD. Nonlinear airfoil torsional response induced by separated flows [Internet]. Proceedings. 2015 ;[citado 2024 abr. 30 ] Available from: https://doi.org/10.2514/6.2015-1423
Vancouver
Pereira DA, Vasconcellos RMG de, Marques FD. Nonlinear airfoil torsional response induced by separated flows [Internet]. Proceedings. 2015 ;[citado 2024 abr. 30 ] Available from: https://doi.org/10.2514/6.2015-1423
Trabalho de evento
An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack (2015)
Zakaria, Mohamed Y.; Pereira, Daniel Almeida; Ragab, Saad; Hajj, Muhammad R; Marques, Flavio Donizeti
Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
ZAKARIA, Mohamed Y. et al. An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack. 2015, Anais.. Reston, VA, USA: AIAA, 2015. Disponível em: https://doi.org/10.2514/6.2015-3166. Acesso em: 30 abr. 2024.
APA
Zakaria, M. Y., Pereira, D. A., Ragab, S., Hajj, M. R., & Marques, F. D. (2015). An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2015-3166
NLM
Zakaria MY, Pereira DA, Ragab S, Hajj MR, Marques FD. An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack [Internet]. Proceedings. 2015 ;[citado 2024 abr. 30 ] Available from: https://doi.org/10.2514/6.2015-3166
Vancouver
Zakaria MY, Pereira DA, Ragab S, Hajj MR, Marques FD. An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack [Internet]. Proceedings. 2015 ;[citado 2024 abr. 30 ] Available from: https://doi.org/10.2514/6.2015-3166
Trabalho de evento
Influence of structural nonlinearities in stall-induced aeroelastic response of pitching airfoils (2014)
Pereira, Daniel Almeida; Vasconcellos, Rui Marcos Grombone de; Marques, Flavio Donizeti
Source: Proceedings. Conference titles: International Conference on Structural Dynamics - EURODYN. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
PEREIRA, Daniel Almeida e VASCONCELLOS, Rui Marcos Grombone de e MARQUES, Flavio Donizeti. Influence of structural nonlinearities in stall-induced aeroelastic response of pitching airfoils. 2014, Anais.. Porto, Portugal: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2014. Disponível em: https://repositorio.usp.br/directbitstream/f8ac4f6e-af7f-4ff6-94a6-3ca03485f916/PROD_25657_SYSNO_3123954.pdf. Acesso em: 30 abr. 2024.
APA
Pereira, D. A., Vasconcellos, R. M. G. de, & Marques, F. D. (2014). Influence of structural nonlinearities in stall-induced aeroelastic response of pitching airfoils. In Proceedings. Porto, Portugal: Escola de Engenharia de São Carlos, Universidade de São Paulo. Recuperado de https://repositorio.usp.br/directbitstream/f8ac4f6e-af7f-4ff6-94a6-3ca03485f916/PROD_25657_SYSNO_3123954.pdf
NLM
Pereira DA, Vasconcellos RMG de, Marques FD. Influence of structural nonlinearities in stall-induced aeroelastic response of pitching airfoils [Internet]. Proceedings. 2014 ;[citado 2024 abr. 30 ] Available from: https://repositorio.usp.br/directbitstream/f8ac4f6e-af7f-4ff6-94a6-3ca03485f916/PROD_25657_SYSNO_3123954.pdf
Vancouver
Pereira DA, Vasconcellos RMG de, Marques FD. Influence of structural nonlinearities in stall-induced aeroelastic response of pitching airfoils [Internet]. Proceedings. 2014 ;[citado 2024 abr. 30 ] Available from: https://repositorio.usp.br/directbitstream/f8ac4f6e-af7f-4ff6-94a6-3ca03485f916/PROD_25657_SYSNO_3123954.pdf

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